Postdoc: High Performance Solution of Three-Dimensional Nonlinear Transient Aeroelastic Problems

博士后：三维非线性瞬态气动弹性问题的高性能解决方案

• 批准号: 9503301
• 负责人: Charbel Farhat
• 金额: $ 4.62万
• 依托单位: University of Colorado at Boulder
• 依托单位国家: 美国
• 项目类别: Standard Grant
• 财政年份: 1995
• 资助国家: 美国
• 起止时间: 1995-06-01 至 1998-05-31
• 项目状态: 已结题
• 来源: https://www.nsf.gov/awardsearch/showAward?AWD_ID=9503301&HistoricalAwards=false
• 关键词: Postdoc; Performance; Solution; Three; Dimensional

9503301 Farhat The accurate prediction of aeroelastic phenomena is essential to the design of safe high performance aircraft. This prediction requires solving simultaneously the appropriately coupled fluid and structural equations of motion. Therefore, numerical aeroelastic simulations are in general resource intensive. We propose to develop high performance methodologies for the parallel simulation of three-dimensional transient aeroelastic problems on advanced homogenous and heterogeneous hardware architectures. More specifically, we intend to develop mixed partitioning procedures for the parallel space and time integration of the governing coupled nonlinear partial differential equations, and investigate their merits in terms of accuracy, stability, heterogeneous computing, I/O transfers, subcycling, and parallel processing. This research is multidisciplinary and includes four components: computational structural mechanics, computational fluid dynamics, applied mathematics and numerical analysis and, computer sciences and parallel processing. The first two components involve the development of discrete mathematical models based on finite elements and finite volumes for representing aerospace structures as assemblies of beams, plates, and shells, and modeling high speed flows around them. The third component addresses the design of staggered and efficient time-integrators for advancing the solution of the governing coupled semi-discrete equations. The last research component aims at exploiting the capabilities of homogeneous and heterogeneous parallel systems to significantly reduce the overall simulation time of these very compute-intensive engineering applications.

9503301 Farhat气动弹性现象的准确预测对于安全高性能飞机的设计至关重要。 这种预测需要同时求解适当耦合的流体和结构运动方程。 因此，数值气动弹性模拟一般是资源密集型的。我们建议开发高性能的三维瞬态气动弹性问题的并行模拟方法，先进的同质和异构的硬件架构。更具体地说，我们打算开发混合分区程序的并行空间和时间集成的控制耦合非线性偏微分方程，并调查其优点的准确性，稳定性，异构计算，I/O传输，子循环，和并行处理。 这项研究是多学科的，包括四个组成部分：计算结构力学，计算流体动力学，应用数学和数值分析，计算机科学和并行处理。 前两部分涉及基于有限元和有限体积的离散数学模型的开发，用于将航空航天结构表示为梁、板和壳的组件，并对它们周围的高速流进行建模。 第三个部分涉及交错和高效时间积分器的设计，以推进控制耦合半离散方程的求解。 最后一个研究部分的目的是利用同构和异构并行系统的能力，显着减少这些非常计算密集型的工程应用程序的整体仿真时间。